Year
1979
Manufacturer
Model
Serial Number
11540
Condition
Used
Registration #
N67CG
FlightRules
IFR
Based at
KBCT
Description
The 1979 Twin Commander 690B II is a proven high-performance turboprop renowned for its speed, reliability, and versatility. Designed for both business and personal travel, it offers excellent short-field capability, efficient operating economics, and a spacious, comfortable cabin. Equipped with powerful Honeywell TPE331 engines, the 690B II delivers impressive cruise performance, range, and climb rates, making it a standout in its class. With its rugged build quality and enduring reputation, this aircraft remains a dependable choice for operators seeking a balance of performance, comfort, and value.
This 1979 Turbo Commander 690B II is ready for its next owner. Reliable, well-maintained turboprop with modern avionics and excellent pedigree.
Highlights:
- Like-new paint - exceptional exterior condition
- Garmin avionics package - modernized panel with advanced capabilities
- Avidyne integration - enhanced situational awareness and navigation
- Fresh 5-year inspection - completed and compliant
- Luxurious leather interior - comfort throughout the cabin
- Keith Freon air conditioning - reliable climate control system
- Always hangared - preserved in pristine condition
- No damage history - clean, well-documented record
- Q-Tips propellers - efficient, low-time props installed
- Super Spar - front wing spar reinforcement
Pressurized
Yes
Additional Equipment
Standard Equipment (690B II)
Instrumentation:
Airspeed indicator (knots only), turn and bank indicator, outside air temperature gauge, aileron trim gauge, dual engine oil pressure and fuel pressure gauges, dual turbine inlet temperature gauges, dual fuel flow indicators with totalizer, hydraulic pressure gauge, dual volt-ammeter, aircraft hour meter, cabin altitude and differential pressure gauge, rapid response vertical speed indicator, magnetic compass, gyro pressure gauge, cabin rate of climb indicator, dual engine oil temperature, RPM, and horsepower gauges, fuel quantity gauge, flap position gauge, propeller de-ice ammeter, and elevator/rudder trim gauge.
Co-pilot’s flight group includes: airspeed indicator (knots), clock, turn and bank indicator, artificial horizon, directional gyro, altimeter, and electric trim release.
Electrical & Systems:
Two 48-amp batteries, two 300-amp starter generators, electroluminescent main switching panels, position lights, belly-mounted rotating beacon, Whelen 3-point strobe system, two auxiliary electric fuel pumps, MIL-H-83282 hydraulic system, aft fuselage avionics access doors, Cleveland power brakes, gear warning horn and silencing switch, electric vacuum pump for outflow valves, two-speed windshield wipers, automatic horsepower limiting system, voltage protection, auto-timed baggage compartment light, two wing-mounted landing lights, vertical fin flashing beacon, taxi lights on main gear, static discharges, electric fuel shutoff valves, dual engine-driven hydraulic pumps, electric hydraulic shutoff valves, deep tinted inner windows, power steering, variable-rate pressurization controller, stall warning horn, wheel well doors, and heavy-duty tubeless main gear tires.
Airframe & Powerplant:
Independent pilot and co-pilot pitot/static systems, external power plug with overvoltage protection, adjustable instrument panel floodlights, electric hydraulic pump, emergency braking system, windshield and side window defog systems, automatically retractable cabin step with spring-loaded link, minibar, heavy-duty locks for main and luggage doors.
Environmental Control System:
Engine bleed air used for pressurization and air-conditioning with water separator, electrical firewall shutoff valves, and cabin depressurization aural warning. Standby 22 cu. ft. oxygen system with individual automatic drop-out constant flow outlets and masks for passengers, quick-donning diluter demand crew masks with mic and purge, and quick filler port. Equipped with Freon air conditioning.
Propellers:
Three-blade Hartzell Q-Tip constant-speed, full-feathering, reversible, heavy-blade propellers (new 2010) with synchrophasing system.
Annunciators:
AC volts, dual chip detection, dual engine inlet heat, low fuel, prop sync, max flow, dual ignition override, dual buss off, dual NTS test, autopilot disconnect, landing gear position, left/right engine fire detection, dual beta mode, dual generators, cabin/baggage door unlatched, low cabin pressure, regulated pressure, dual horsepower limiting off, environmental control master, and electrical system voltage.
Ice Protection:
Heated stall warning detector, electric inlet heaters for generators, wing and empennage pneumatic de-icing boots, dual static sources (heated pilot side), electric rudder horn slot heaters, electrically heated windshields, fuselage ice shields, dual heated pitot tubes, left/right wing ice lights, electric propeller de-icing, and rudder tab heater.
Miscellaneous Equipment Provided with Aircraft
Rudder gust lock, internal control lock, pilot operating handbook, combination tow bar and tail stand, cabin door hold-open device, engine tailpipe covers, pitot covers, fuel sampling cup, throw rugs, touch-up paint kit, engine inlet covers, and pilot checklist.